Method for repairing fuel nozzle guides for gas turbine engine combustors using cold metal transfer weld technology

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United States of America Patent

PATENT NO 9995487
SERIAL NO

14684465

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Abstract

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A fuel nozzle guide for a combustor of a turbine engine includes an annular base with a hub section, the hub section at least partially formed of a Cold Metal Transfer (CMT) weld and a method and system therefor.

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Patent Owner(s)

  • UNITED TECHNOLOGIES CORPORATION

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Rose, William M Warren, US 26 95

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